SYSTEM FOR SUPPLYING FUEL TO A COMBUSTOR
    31.
    发明申请
    SYSTEM FOR SUPPLYING FUEL TO A COMBUSTOR 审中-公开
    向燃油供应燃料的系统

    公开(公告)号:US20140174090A1

    公开(公告)日:2014-06-26

    申请号:US13723322

    申请日:2012-12-21

    CPC classification number: F23R3/28 F23R3/14 F23R3/286 F23R3/346

    Abstract: A system for supplying fuel to a combustor includes a combustion chamber and a liner that circumferentially surrounds at least a portion of the combustion chamber. A plurality of fuel nozzles are radially arranged across the combustor upstream from the combustion chamber to supply a swirling flow of fuel into the combustion chamber. A first fuel injector downstream from the plurality of fuel nozzles provides fluid communication for fuel to flow through the liner and into the combustion chamber. The first fuel injector is circumferentially clocked with respect to the swirling flow of fuel in the combustion chamber.

    Abstract translation: 用于向燃烧器供应燃料的系统包括燃烧室和周向围绕燃烧室的至少一部分的衬套。 多个燃料喷嘴沿着燃烧室上游的燃烧器径向布置,以向燃烧室供应涡流。 从多个燃料喷嘴下游的第一燃料喷射器提供流体连通以使燃料流过衬套并进入燃烧室。 第一燃料喷射器相对于燃烧室中的燃料的旋转流沿圆周方向计时。

    SYSTEM FOR COOLING A HOT GAS COMPONENT FOR A COMBUSTOR OF A GAS TURBINE
    32.
    发明申请
    SYSTEM FOR COOLING A HOT GAS COMPONENT FOR A COMBUSTOR OF A GAS TURBINE 审中-公开
    用于冷却气体涡轮机燃烧器的热气体组分的系统

    公开(公告)号:US20140130504A1

    公开(公告)日:2014-05-15

    申请号:US13674255

    申请日:2012-11-12

    Abstract: A system for cooling a hot gas path component for a combustor generally includes an impingement sleeve that circumferentially surrounds an outer surface of the hot gas path component. A first cooling chamber is defined between the impingement sleeve and a first portion of the outer surface of the hot gas path component. A second cooling chamber is disposed downstream from the first cooling chamber. The second cooling chamber is defined between the impingement sleeve and a second portion of the outer surface of hot gas path component. An inlet extends through the impingement sleeve so as to define a first flow path into the first cooling chamber. An outlet defines a second flow path between the first cooling chamber and the second cooling chamber.

    Abstract translation: 用于冷却用于燃烧器的热气体通道部件的系统通常包括围绕热气体通道部件的外表面的冲击套筒。 第一冷却室限定在冲击套筒和热气体通道部件的外表面的第一部分之间。 第二冷却室设置在第一冷却室的下游。 第二冷却室限定在冲击套管和热气体通道部件的外表面的第二部分之间。 入口延伸穿过冲击套筒,以限定进入第一冷却室的第一流动路径。 出口限定第一冷却室和第二冷却室之间的第二流动路径。

    VESSEL APPARATUS WITH FLOW CONTROL ELEMENT
    33.
    发明申请
    VESSEL APPARATUS WITH FLOW CONTROL ELEMENT 有权
    具有流量控制元件的船舶设备

    公开(公告)号:US20130292390A1

    公开(公告)日:2013-11-07

    申请号:US13875510

    申请日:2013-05-02

    Inventor: Lishun Hu Wei Chen

    CPC classification number: F17C13/002 F16J12/00

    Abstract: A vessel apparatus includes a pressurized vessel and at least one flow control element. The at least one flow control element is located within the pressurized vessel and has an upwardly-converging wall.

    Abstract translation: 容器装置包括加压容器和至少一个流量控制元件。 至少一个流量控制元件位于加压容器内并且具有向上会聚的壁。

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